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Lateral Stability Characteristics Between Mach Numbers of 0.80 and 1.57 and Simulation of Coupled Motion at Mach Number of 1.30 of a Rocket-propelled Model of an Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces
Document ID
19930090203
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
D'Aiutolo, Charles T
Henning, Allen B
Date Acquired
August 16, 2013
Publication Date
April 10, 1956
Report/Patent Number
NACA-RM-L56A17
Report Number: NACA-RM-L56A17
Accession Number
93R19493
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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